NASA Johnson Space Center
Oral History Project
Commercial Crew & Cargo Program Office
Edited Oral History Transcript
Frank L.
Culbertson
Interviewed by Rebecca Wright
Hawthorne, California – 4 June 2013
Wright: Today is June 4, 2013. This oral history interview is being
conducted with Frank Culbertson at the Headquarters of the Orbital
Sciences Corporation in Dulles, Virginia, for the Commercial Crew
& Cargo Program Office History Project. Interviewer is Rebecca
Wright, with Rebecca Hackler.
Mr. Culbertson serves as the company’s Executive Vice President
and is also General Manager of Orbital’s Advanced Programs Group.
He is responsible for the execution, business development, and financial
performance of the company’s human spaceflight and national
security satellite activities. Thanks again for taking time out of
a very busy morning.
We know that you spent about 18 years with NASA before you left the
space agency and went on to another career. Could you share with us
briefly where that took you, how you ended up with Orbital, and why
you chose to be here?
Culbertson:
I left NASA in August of 2002 and went with SAIC [Science Applications
International Corporation]. My first job with them was Program Manager
for the safety contract at Johnson Space Center, which supported all
the [Space] Shuttle and [International Space] Station operations.
It had about 550 people on the program at that time, but it’s
much smaller now with the retirement of the Shuttle.
I spent a couple of years in that job, then I moved on to be the business
unit manager for all the NASA human spaceflight business, as well
as some of the environmental sciences such as the National Data Buoy
Center, the atmospheric research, things like that that SAIC was doing.
Then I spent a year as the Program Director for all of the global
climate change programs in the company.
I left SAIC in 2008 and joined Orbital in August of 2008, and I’ve
been here ever since. Initially I was Deputy General Manager responsible
for all the human spaceflight systems in the company, including the
cargo resupply service, and efforts that we made in other areas. Then,
last September, I was asked to take over the whole business unit,
the Advanced Programs Group, as General Manager. I still have the
human spaceflight, and it also includes all of our national security
space systems.
Wright:
Busy man. Today we’ll only talk about one piece of it. When
you came here, the work had already begun on the COTS [Commercial
Orbital Transportation Services] program. Tell us what your first
thoughts were, because this is a different way of doing business with
the government.
Culbertson:
Right. I’d actually been exposed to it a couple of years prior,
when [G.] David Low was here. He was managing the effort to try to
capture that business on the first round of COTS awards under the
Space Act Agreement.
Orbital had a plan, that he had shared with me a little bit, and we
were actually subcontracted to them for a piece of the work on the
safety side. That was to provide cargo delivery based on a Russian
system, similar to a Progress [spacecraft], but still using the Antares,
what was then called the Taurus II launch vehicle. Orbital had begun
development of the Taurus II on its own, prior to any cargo efforts,
because we saw the need for a medium-class launch vehicle to replace
the Delta II that was being retired.
Orbital was not selected on the first round of COTS. SpaceX [Space
Exploration Technologies Corp.] and Rocketplane Kistler were selected,
and about a year later, RpK did not meet their milestones and NASA
dropped them. It’s a lot more complicated than that, but that’s
it in a nutshell. NASA had already spent about $32 million on them,
so they had the amount that they had initially given to them and SpaceX,
minus $32 available. Orbital put in another bid and was then selected
for the COTS demo [demonstration] mission. Because of the lower amount
of money and the shortened timeline that they wanted us to attempt
to achieve, we only planned on doing one demo mission prior to beginning
any cargo delivery, assuming that a contract would be let at some
point.
We started almost two years behind SpaceX in developing the on-orbit
system. This was in February of 2008, and then when I came on board
in August we had already submitted the first round of proposals on
the cargo [Commercial] Resupply Services [contract]. They there were
doing best and final, and I was involved in some of the final reviews
on that. We submitted in October, and then were selected in December
for the actual cargo resupply service, along with SpaceX. There was
a protest by a third competitor that went on for quite a while, but
finally was resolved in our favor. In the meantime, NASA had us continue
working. They had the option to either stop work or continue work,
but because of the fact that they really wanted cargo capability,
they told us to go ahead and continue.
They were going at some risk, but it all worked out in the end. At
the time that they awarded us the contract, our plan was to fly an
Unpressurized Cargo Module [UPCM], because it was a little less expensive
to demonstrate the capability to approach the Station and do a good
rendezvous using our Service Module with an empty UPCM on the front
end. When they awarded us the contract, all of our flights, our missions,
were for pressurized cargo. At that time, after a lot of discussion
internally and some with NASA, we decided to change our plan from
Unpressurized to a Pressurized Cargo Module on the demo mission, which
required some investment on the company’s part. We felt that
that was what we were going to be delivering, so we needed to demonstrate
it on the first mission.
We worked with our supplier, Thales Alenia [Space], in Torino, Italy,
and started the work on the PCM [Pressurized Cargo Module]. The Service
Module itself is kind of the heart of the system, and that has been
developed here at Orbital, based somewhat on our legacy of geostationary
satellites that we’ve built for many years. It turns out it’s
a lot more complicated and a slightly different design, but some of
the basics, such as propulsion and power systems, are similar to our
geos.
That development was ongoing, and so we basically had three things
occurring at the same time. One was the spacecraft development, essentially
what the Space Act Agreement was covering was development of the spacecraft.
That initial amount was $170 million, and then Orbital’s investment
was going to be everything beyond that. Earlier on, it was a much
smaller number than it is now. The rocket [Taurus II/Antares] was
being built under Orbital’s own internal research and development
funds, and that’s grown over time too, and of course the schedule
is stretched out. Then, the third piece of the puzzle was the launch
site itself.
Before I came on board, Orbital had selected Wallops Flight Facility
or Wallops Island [Virginia] as the launch site, after doing a basic
competition between Virginia and the State of Florida on the commercial
launch facilities. We were basically required by the Space Act Agreement
to do the negotiations and come with that capability, but we were
starting from a green field. There was a slab of concrete where we
were intending to launch from, and that was pretty much it. Working
with the Mid-Atlantic Regional Spaceport [MARS]—which is under
the Virginia [Commercial] Spaceflight Authority, who had hoped to
bring in Maryland and North Carolina and Delaware and other Mid-Atlantic
states, and Wallops Island and NASA, and with some support from Congress—we
began the effort on developing the pad.
It was the responsibility of MARS, as we call it, to actually develop
and build and test the pad, but we worked hand-in-hand with them because
it was designed to support our rocket initially. Now it’s designed
to support multiple versions, multiple users. Right now we’re
the only user, so they’ve been focused on our needs. NASA was
supportive of this because they were going to get a new liquid rocket
launch capability out of it, a new launch pad on the East Coast that
theoretically would not be conflicting with anything in Florida, but
would give the country another site to launch medium-class rockets
from.
They built the Horizontal Integration Facility, which initially was
going to be a MARS facility but NASA decided they would do that and
own it, and they still do own it. We provided a lot of engineering
support and actually some investment on our side in the pad. All of
that’s a matter of record, but it became a fairly complicated
three-way management process that we had to work through. You had
senior people on all three sides that were trying to influence things
and move things forward. For the most part, people worked together
fairly well, but whenever you’re worried about money and budgets
are growing, you end up eventually getting down to the last few million
dollars, and who’s going to pay for that? So, we had a lot of
intense discussions over the last few years. The schedule at the pad
ended up driving the program more than anything else.
There were other issues we were having to work at the same time, but
they were masked somewhat by the pad issues. The pad ended up being
the long pole. We probably ended up about two years beyond our initial
estimate of first launch, maybe a year and a half, by the time we
finally launched. A lot of that had to do with designing the fueling
system, which turned out to be a lot more complex than folks had estimated
on the Virginia side for the liquid oxygen, the kerosene, all of the
gases such as helium and nitrogen that had to control the systems
and provide pressurization. It’s all controlled by software,
it has to all happen on a schedule at a certain time, in a certain
sequence, at the right temperature, the right pressure, etc. It’s
fairly complicated, and that had to go through a lot of testing.
In the meantime, we were working issues with the rocket itself. The
engines that we are using are AJ-26 engines that were originally built
in Russia by a company called NDK, then SNTK, and now Kuznetsov [Design
Bureau], who developed this engine for the N-1 Moon rocket that the
Soviets were building back in the ’60s. It was going to have
40 of them at a time on the rocket. It had four launches but no successful
flights, primarily due to structural and guidance issues, not due
to the engine.
The engine is actually one of the most highly-tested in terms of total
test time of any engine that’s ever been built, in terms of
thousands of seconds of testing, really hours of testing. It’s
fairly well understood, and seemed to be robust. It certainly had
enough thrust for two of them to provide us our access to orbit. Aerojet
bought 37 of them back in the ’90s, and they were originally
going to be used by Kistler on their planned launch vehicle. One of
them was actually tested fairly extensively for that purpose, but
then they went under and the engines were put in storage.
After evaluating all options, Orbital decided that these were the
most readily-available engines in the U.S. because there was no U.S.
manufacturer building engines in this class anymore, which is unfortunate.
The only other competing engine is being used by ULA [United Launch
Alliance] under the import license of RD AMROSS and Pratt & Whitney
[Rocketdyne] on the Atlas V [rocket]. They have established an exclusive
right to those engines so nobody else is allowed to use them, which
makes it difficult to compete. That’s a whole other story you
could evaluate.
Aerojet began bringing the engines out of storage, refurbishing them,
adding the components to Americanize them basically, such as thrust-vector
control, and electronic throttle control. We began testing them at
[NASA] Stennis Space Center [Mississippi], which we also had a [reimbursable]
Space Act Agreement with for engine acceptance testing. I believe
it was the fourth one that we were taking through the tests when we
had a test failure, and the fuel manifold line basically split apart.
We shut the engine down immediately, so there was no significant damage
to the test stand or even to the engine itself, except for that manifold
line.
That was a major issue for us, and it turned out that that engine
had a crack in it that was not detected by Aerojet. It resulted in
stress corrosion cracking that grew under pressure, and it basically
unpeeled the pipe and spilled fuel, which caused a small fire but
no major damage. That of course brought the test program to a stop,
and we spent a lot of time evaluating and then doing some additional
tests in Russia.
Actually, before that we had a test failure in Russia on a similar
engine, not exactly the same. They were testing at a high power setting
and we believed, due to an instability in the fuel control, they ended
up having a turbo pump separate from the engine. However, that was
prior, and then they fixed that problem, and then we went on with
our testing. The engines have had some issues going forward, but we
and Aerojet worked together to come up with a nondestructive evaluation
program where we do X-rays and eddy current inspections, ultrasound
inspections, to find where the cracks are. Then they’re repaired
by welding.
So far the welded engines have performed fine, and they appear to
have found all the cracks in the ones that have any. One or two engines
came through clean, but most of them have at least one or two cracks
that have to be repaired, just in the interest of caution, to be conservative.
That set us back a little bit in the engine development program, but
we got back on track and the cores began arriving from the Ukraine.
They were built by Yuzhnoye [Design Office] and Yuzhmash [A.M. Makarov
Yuzhny Machine-Building Plant], which are the Ukrainian companies
that built the Zenit [rocket] and also built a number of ICBMs [Intercontinental
Ballistic Missiles] for the Soviet government back in the ’60s
and ’70s. They built the missiles that caused the Cuban Missile
Crisis, just as a historical fact.
Wright:
Thank you for that.
Culbertson:
At any rate, they worked closely with us to make sure that the systems
all worked together and did their own testing and delivered a good
product. They began arriving by large cargo ship into Wilmington,
Delaware. The whole process of getting those cores, which are probably
close to 100 feet long and four meters in diameter, through Delaware
and Maryland down to Virginia is quite an operation in itself, and
probably worth a whole article. In fact, there have been some articles
written about it because it’s an Articulated Lowboy [truck]
that has to be steered around corners with a rear steering wheel and
a front steering wheel. These guys are very good at it, but they go
very slow through these little towns, and they do not go on the freeways.
It’s quite an entertainment factor for the locals there.
That’s worked out, and we now have, including the one that we
just launched—I believe we now have five cores in the country.
As all of that was going on, in parallel, we were continuing to develop
and built the Cygnus spacecraft. The Pressurized Cargo Module went
very smoothly, working with Thales Alenia [Space], and they began
building them right away.
We placed all nine of them on order right away. They just started
building them on the right frequency, and they’ve done a really
good job with them. The first one actually arrived almost two years
ago at Wallops, and it’s sat in storage since then. The service
module itself, as I said, was based on our prior satellites, but much
more complex. Like the Shuttle, it had to have significant redundancy,
at least triple if not quad [quadruple] in some cases, because it
needed to be human-rated in the vicinity of the Space Station.
It was planned to do an autonomous rendezvous. We would monitor it
of course, as would NASA, fly up the R-bar [vector from Station to
the center of the Earth] to the Space Station under its own control,
and then stop 10 meters from the Station automatically. All of that
had to be redundant and very carefully managed, so it required a lot
of testing. The design had to be reworked a couple of times, as we
discovered how complex this was compared to everything Orbital had
done in the past. We kept NASA in the loop on everything we were doing.
We were perfectly transparent to them. They attended all our reviews,
and occasionally we would have helpful comments and suggestions. Occasionally,
we would go to them for consultation if we ran into a difficult problem.
Along the way we had to brief a number of reviewing panels, such as
the ASAP [Aerospace Safety Advisory Panel] and the NAC [NASA Advisory
Council] and other safety groups and review panels, but we did not
have the same level of oversight that NASA would normally have on
a NASA-owned program. We own the spacecraft and the design, and we
were going to provide them with a service. They had a great deal of
interest in how it operated near the Station, of course.
In fact, they had a lot of interest in how it operated from beginning
to end, but early on in my job overseeing all of this, I had several
discussions with senior NASA folks and mid-level folks about, “I
appreciate your suggestions, but it’s our design, and we’ll
make our own decisions on the PDR [Preliminary Design Review] and
CDR [Critical Design Review] and decide what’s the safest, most
efficient, and cost-effective approach. Thanks for your input.”
Wright:
Was that a defining moment between the Space Act Agreement, compared
to a traditional contract?
Culbertson:
This was still during the development for the Space Act Agreement
because again, it was our spacecraft, not theirs. As they like to
say, they were an investor in it, and so they had a vested interest.
They wanted us to succeed so that we could begin delivering hardware,
but at no time was it ever intended for any of this hardware to be
handed over to NASA like we would in the past. Even satellite science,
our communications satellites, are delivered to the customer on-orbit,
and there’s signatures associated with that.
This one is never delivered to anybody, we just deliver the cargo.
It’s the same as putting a package on a UPS [United Parcel Service]
truck and having it go to somebody’s house. You don’t
ever own the truck, you just count on the package getting there. That
was a defining moment where we had to make sure everybody understood
their own boundaries and what was appropriate and what wasn’t.
It’s worked very well.
Alan [J.] Lindenmoyer’s [Commercial Crew and Cargo Program]
Office, particularly Bruce [A.] Manners [NASA COTS Project Executive],
have been great to work with. They are very similar to the Shuttle-Mir
Program Office in that they’re very small, they’re very
focused on what they need to do, they don’t have a lot of bureaucracy
associated with what they’re doing. They’re very good
at listening and providing advice and insight, but they don’t
interfere, particularly once we set the rules.
The ISS Program is like the ISS Program was to the Shuttle-Mir Office,
in that it’s much larger with a lot more attempts to be involved,
and of course a lot more requirements to meet. They started imposing
themselves early on because the demo was going to the Station, and
we did have to meet their requirements. They are a much bigger bureaucracy,
but still very good to work with and have been very helpful. Kathy
[Kathryn L.] Lueders was the [Transportation Integration Office] Program
Manager on their side, until she moved to a new job, and now Dan [Daniel
W.] Hartman is there. They both have been very easy to work with,
and we’re all pulling in the same direction on all of this.
They have a contract they have to manage, and we have to manage our
side of it. We occasionally get into the normal business disputes
over things, but it’s not acrimonious by any means. As we went
through the development of the Cygnus, there were always challenges,
and lots and lots of testing that had to go on, and problems to overcome
such as sticky latch valves, software that didn’t work exactly
right. We had some graduation exercises we had to get through in order
to say that, yes, we really were ready to go to the ISS, including
joint tests with the NASA simulators, with our system, our actual
hardware, to ensure that it all played together and operated as designed.
Then, we had to get through the Safety Review Panel [SRP]. As a vehicle
carrying payloads to the Station, we had to satisfy all their requirements.
Eighty percent of the effort to get through the SRP was based on collision
hazard and closing that hazard out. You can get the details on our
competition and where they got to, and how long and how close they
were to launch. We finished the Joint Test 4, as we call it, which
satisfied all the software requirements about three months ago, so
essentially four to six months ahead of flight.
We completed the SRP about two months ago, so we’ve satisfied
all of their requirements there and we don’t really have any
open issues. We just need to get the launch and get to the Station.
When we briefed the Aerospace Safety Advisory Panel and the [Thomas
P.] Stafford Commission jointly, the feedback we got was, “Now
we’re hearing stuff we understand. You guys came in and you
talk like aerospace engineers. You speak NASA, and you’re well
organized.” They really appreciated it.
We made it through those reviews fine, and they could see that we
really did have our act together. We just don’t make a lot of
noise about it. Our folks are very proud of being professional, being
on time, getting the job done correctly. I got feedback from our very
first trip to Houston to work software. Our guys showed up well-dressed,
in lab coats, and working with the NASA folks. Had a test plan ready
to go, not everybody does that. Then when we briefed the review panels,
of course we showed up in coats and ties, and we had a clear PowerPoint
[presentation]. We knew how to communicate with them, and it also
indicated that my program managers and our leads were managing things
well. They had a good handle on the issues.
But, spaceflight’s hard, so we’ve been working through
all the challenges to get to where we are. A key decision we made
early on was to try to keep the production going in order to meet
the original intent of the contract, right from the very beginning.
We knew there would be delays in the demo because of launch vehicle
and launch pad issues. We were ready to go on the demo over a year
ago, spacecraft-wise and PCM-wise, but the pad was slowing us down.
We kept working, kept the team producing the next spacecraft, so we
actually have five spacecraft in various stages of production. Three
of them are complete, and two more are going through assembly, and
we’ll have more coming about every four months. Our intent was
to make sure that regardless of what delay we had up front, we could
meet the period of performance to the contract to complete by the
end of 2016, which is when the contract expires.
If we don’t launch by the end of 2016, NASA’s going to
have to reopen the contract and renegotiate with us because prices
will change, various other things will have to change. What they would
do in that case is force us to slow down, which means I’ve got
to take people off the contract, and there’s no guarantee they’ll
come back if I have to either lay them off or reassign them. I’m
trying to keep things going at the pace we were originally contracted
for. We don’t have total agreement from NASA that that’s
what they’re willing to support or do. However, I’m trying
to protect the situation that some of the other cargo providers may
not always be there, so if somebody else falters, we can fill in.
We actually do have a task order that requires a launch “on
need,” meaning they can call us up on a six-month call, and
we could launch as much as three months early. So we’re building
to support that. We’re actually building a little faster than
that so we can support a much higher flight rate. I think in the end
they’ll need it, but they’ve got budget pressures. They’re
being criticized by the [NASA] Inspector General for paying us without
having flown our demo mission, which puts them in an awkward situation.
The problem is that the folks writing those criticisms don’t
understand how commercial business works. If you don’t pay periodic
milestone or installment payments, you can’t do the production
unless you go take out business loans, which adds to the expense of
the whole project because you’ve got to pay interest on them.
If the government pays progress payments, then we can keep the production
going and then we’re ready, at the end, to launch whenever they
say.
We’ll have hardware ready to go probably before they’re
ready to receive it, but that’s a better position than having
us wait on it. We feel bad about being late on the demo mission, but
we’re ready to go with everything beyond that, and we think
it’s important to be in that position, which demonstrates we
have the capability to do a lot of stuff in parallel. That’s
not always the case with other providers. All of the components for
the first three missions are essentially ready to be gathered at Wallops.
Not all of them are there just because of space limitations, but we
can move them in every two or three months as need be. The others
are on track to meet all of our needs on a fairly aggressive schedule.
If NASA needs us, we’ll be there.
Getting the [Antares] test flight off was a major step for us because
NASA had decided to withhold cash payments to us on certain things
until we flew the test flight, because of the criticism they were
receiving from politicians and others. They’re very sensitive
to that obviously. There would be certain elements of the space community
in favor of what we’re doing, but others are totally against
it, and then there’s others who would like to just see us go
away. They’re trying to balance all of that, so we had to delay
some payments for a while. Once we flew the test flight, they did
in fact pay us for things they’d already ordered from us. We’re
concerned that they’re going to respond to that kind of pressure
again in the future, and we’re going to be cash poor.
We’re actually significantly negative cash on this program because
NASA has a higher percentage of payment holdback, despite the fact
that they’ve got a schedule that starts two to two-and-a-half
years ahead of launch of paying us, it never totals more than—I
don’t know if I can say the number or not, but it’s only
a percentage of the actual cost of the mission until we actually get
to the Station. We’ve got a lot at risk until we actually launch
and get to the Station, and neither the press nor the politicians
seem to be able to understand that, no matter how many times I explain
it.
NASA is paying us on a fairly aggressive schedule so that we can maintain
one, but they’re not paying us what we’re spending, so
we’re significantly cash negative until the very end of the
program. We are taking a significant risk. The other aspect that people
don’t seem to understand is that if we were to stop producing,
or to walk away from this, or be terminated, we would owe NASA significant
amounts of money that they have paid us already. It’s certainly
not a low-risk proposition for the company to do this on a commercial
basis.
People might ask, “Why are you doing it if there’s no
profit upfront and very little profit at the end?” That’s
because this is only for the first eight missions. The Station has
been forecasted to continue to at least 2020, maybe 2028, so as we
get better and more efficient at production and NASA has a higher
and higher need for cargo, there should eventually be a fairly profitable
business there.
It’s not going to be wildly profitable—it’ll always
have low margins because it’s NASA—but there will be some
positive for the company. It’ll allow us to continue building
Antares rockets that can be used for other purposes, and we’ll
establish a track record that we think will be attractive to other
users. The Cygnus itself can be used for other purposes, too.
Wright:
Are you already looking for those potential customers?
Culbertson:
We’ve been looking for them for a long time, but partly because
of the nature of this endeavor, and maybe the facts of some of our
hardware—and we don’t market the same as other folks.
We’re not going to promise something we can’t be certain
we’re going to deliver. We don’t have any other orders
yet for the Antares. We’ve had lots of feelers, lots of inquiries,
but I think until we actually get the demo flown and get to the Station,
it’s going to be hard to convince people.
We’ve also been hit with a double whammy, in that budget cuts
and the sequestration hit at a very bad time, where people are not
able to commit funds for new programs right now. We had anticipated
a number of things coming our way by this summer, but the situation
being what it is, particularly in the DoD [Department of Defense],
nobody’s willing to go out on a limb right now. We’re
having to wait until all of this passes and people are actually able
to say, “Yes, that’s the right size we need and you can
fly at the frequency we need.”
I think they’re also waiting to see for sure that our engines
will work, because they are 40 years old. They’ve been reworked,
and there were issues during testing. Rightfully, there’s a
little bit of a skepticism, “Is it going to be good for the
long term?” We’ve gained a lot of confidence on the engines
based on recent testing, as well as the test flight itself. The engines
and the core performed superbly. They hit all their numbers. I mean,
we were holding our breath for four minutes there, but it worked and
put us at exactly the right trajectory at the end of the first days
that we were expecting.
We gained a lot of confidence with that. Obviously we have to continue
to keep our eye on the ball for every single flight, but it looks
like the system is going to be on track to be successful. Beyond CRS,
if we want to fly other cargo missions or for other customers, we
do have to increase our supply of engines, so we’re working
with Aerojet as well as other companies on a competitive situation
to provide us with engines beyond CRS.
We have enough to go a few flights beyond CRS, but beyond 2018 let’s
say, we need to have other engines online. There’s time to develop
that and there’s options being explored, such as restarting
the production or a new engine out of another company. The unfortunate
side of that is that the only engines anywhere near that class that
are being produced in the U.S. are the Merlins that SpaceX produces,
and it takes nine of them to meet the need. As far as I can tell,
they don’t have any excess capacity, nor are they interested
in selling them to anybody else.
We have to go overseas to get any engine supply in that class, for
blocks of kerosene. We’re working on all of that. We’re
not sitting on our hands, we’re planning for the future. I’m
fairly confident we’ll have a good solution, and we may have
two solutions. There are a couple of competitors out there that are
looking at ways to provide us with engines. There’s a couple
of U.S. companies that are starting to get more interested in doing
something in the U.S., because I really think we need to expand back
into that capability.
As far as what’s next, the demo mission is planned for August
or September. I don’t know when you’ll be publishing this,
but by the time you do, we’ll hopefully have flown. We’ve
had lots of interesting discussions with the customer on how to execute
a lot of this, and I’m kind of fortunate in that I know all
the players and they know me and we trust each other. We know what
we can argue about and what we can’t. When one side or the other
wants to go a certain direction, we’ve both got it figured out
pretty well ahead of time. We’re able to arrive at solutions
fairly quickly.
I requested the launch-on-need capability for a number of reasons,
and finally the Station Program said, “Yes, that’s probably
a good idea.” They came along, and it kept some milestone payments
on schedule and gave them justification to keep doing that. It’s
a good capability to have if somebody falters. We’re in an interesting
discussion right now on when to launch the next mission.
As it turned out, when we were getting ready to launch the [Antares]
test flight, because we were still delaying a little bit as we went
through the hot fire and the wet dress rehearsal and on and off the
pad, etc., there was a [NASA] mission called LADEE [Lunar Atmosphere
and Dust Environment Explorer] that was supposed to launch this coming
summer. They’re launching on Minotaur [rocket], which we actually
provide the services for. It’s an Air Force orbital launcher,
and it’s also launching out of Wallops at the pad right next
door. We thought, “They’ll launch in August, we’ll
launch in the spring, and in the fall we’ll conflict.”
After we and NASA spent a good bit of money modifying a small facility
up there for fuelling our spacecraft, we found out that LADEE had
declared they were going to use that facility, and that they were
reserving it for four months, which meant we couldn’t get in
there to fuel our spacecraft for the demo mission, which would have
prevented us from launching when we wanted to. We got a call from
NASA—this is the Science Directorate versus the Human Exploration
[and Operations] Directorate—and interestingly, NASA’s
not as well coordinated internally as we would all hope. We end up
being the conduits between the various directorates.
They had just kind of unilaterally declared this, and so the Station
Program got involved. You can imagine their reaction, “You’re
going to do what to our spacecraft?” They ended up asking us
to accelerate our delivery to Wallops, which we did, and they said,
“Can you be in and out of that facility in a week?” I
said, “We can do it in less than that,” and we did. We
had our best people on it. We got in there, we got fuel, and we got
out.
Everything was fine and safe, but then they didn’t show up.
They were delayed but didn’t tell anybody. They thought we were
going to cover for them. They’re not making their August launch
date and because of the amount of work we needed to do after the test
flight, both on the pad and on getting the next rocket ready, we were
slipping into late August, possibly September. They decided they were
going to move into September, right in the middle of our launch window.
That caused another conflict, so we’ve decided we can work some
overtime and we can actually get off by the end of August.
We don’t have complete agreement with all the people involved
that we can launch in August and they can stay on the pad and launch
in September, but I think it’ll work out. However, the Space
Station Program was working an issue with the Japanese on the HTV
[H-II Transfer Vehicle] arrival date. The HTV launches out of Tanegashima
[Space Center], Japan, and the Japanese own the proximity system that
we also use for communications with the Station. We have some of their
hardware, and then there’s hardware on the Station. We can’t
both be there at the same time.
The Japanese have a rule that they need possession of those bandwidths
and that hardware 30 days prior to their launch to get everything
all set up, so we can’t launch or dock during that timeframe.
Then they want to keep it that way for 20 days after undocking. We’re
not sure why that requirement’s there. The Station Program’s
been trying to shorten that. That moved out ability to dock to September
12th, and LADEE wants to launch on September 6th.
I said, “Look, we’re going to be ready on August 29th,
we’re going to launch then, and we’ll just wait on orbit
until you’re ready to receive us.” Of course, that got
everybody all spun up. “No, you have to launch three days ahead
of time and go straight there,” and I said, “No, we don’t
actually.” We don’t have people on board; we don’t
have any perishables on board. We were going to carry some apples
and stuff, but we’ll see.
It’ll give us a chance to both test this system out and give
our team more time, and we can sit there and wait until you’re
ready for us, 1,000 kilometers away. The initial reaction was, “Well,
we’ve never done that before, we can’t do that,”
but eventually we’ve convinced almost everybody that this is
a good idea. Our team loves the idea because first of all, we can
go ahead and get off the pad and get ready for the next one, which
is coming right after it in November or December, and we need the
time to get both the pad and the rocket ready. And it gives us more
flexibility. If the Station does have a problem, we can now prove
that we have the ability to loiter and wait until they’re ready
to receive us.
If we were to launch on time, say, three days ahead, and then right
after we launched they had a failure on a computer, or the arm [robotic
Canadarm] had a problem and they couldn’t grapple us, we could
sit and wait until they fixed it. We know, by analysis, we can wait
at least a month, maybe more, with the fuel we have on board, to actually
make an approach. This gives both sides a lot more flexibility. Once
I got them to calm down a little bit, they actually started liking
the idea on the NASA side. I said, “We can do this on every
mission, basically. We’ll launch when we’re ready, you
take us when you’re ready, and we don’t have to tie the
two dates together so tightly.” If we had something perishable
on board or something that had limited life, batteries or something
like that, we’d have to tighten it up, but we can do it either
way.
This also gets us ready for secondary missions that we might want
to do after undocking. There’s a number of people who would
like to fly other payloads, and we already have contracts for a couple
of them that we will execute after undocking, after we’re safely
away from the Station. One’s a fire experiment with [NASA] Glenn
Research Center [Cleveland, Ohio]. They want to evaluate how fire
behaves in various materials in zero-G [gravity], in an environment
that’s away from people. Eventually they want to look at extinguishing
capabilities. We’ve got a contact for three of these experiments,
starting to work on five. That’ll require staying on orbit extra
time, so we want to make sure we can control the spacecraft and do
all the things we need to do.
That’s going to be a good exercise I think, but we’re
now looking at things we can do after undocking because it’s
a relatively short docked period. See if we can test out other capabilities,
such as a shut off a control system, and see how it does with less
capability. Then eventually reenter it. Of course our spacecraft reenters
and burns up, rather than being recovered.
We actually have a good relationship with a team in [NASA] Langley
[Research Center, Hampton, Virginia] that’s been developing
an inflatable decelerator and reentry system called HIAD. HIAD stands
for Hypersonic Inflatable Aerodynamic Decelerator. Actually, it’s
called HEART [High Energy Atmospheric Reentry Test] now.
They’ve tested it on a sounding rocket on a subscale, but they
want to test it on a full scale. Theoretically, we could fly that
in between our Pressurized Cargo Module and our Service Module. It
takes about a meter, and you separate the two after you exit the orbit
burn, it inflates and it basically is like a wok bowl around the leading
edge. They made a model and I called it my “wocket.”
It gives you a conical leading edge to enter the atmosphere with heat-resistant
material, and it’ll slow you down to basically parachute speed.
We don’t have a parachute installed, but the analysis showed
that it’s large enough and the rubberized fabric is inflatable,
and it actually will bring you down relatively slowly and probably
survive to the surface of the ocean. It might be recoverable, we’ll
see.
Wright:
It would be great to check out how your spacecraft did.
Culbertson:
Well, it could be a lifeboat for the crew if we ever get to that point.
We’re looking at all kinds of possibilities to both justify
additional work up there as well as looking, since we’re a business,
for revenue-generating things to do too. Also to service the Station,
because the long-term goal is to go beyond low-Earth orbit and use
the Station as a test pad for all kinds of hardware and technologies
that will support going to the Moon and on beyond that.
We think our system will support people in lunar orbit. Even on the
surface, we could deliver cargo to L2 [Lagrange point]. We’ve
already established that very clearly with a team at JSC, and they
like our spacecraft for that purpose. We have to add a little more
fuel and maybe some more shielding, but it’s designed for 15
years of life, based on our geos [geostationary satellites], so it
can stay in orbit a long time. You could even make a habitable module
out of it if you put in a life support system. It’s very similar
to the MPLM [Multi-Purpose Logistics Module], just smaller.
We’re looking to the future, and we think it’s important
that we provide this cargo service to the Station so that it can remain
viable and remain on orbit indefinitely, and that they can have six
or seven people up there. Without our cargo capability they can’t
do that, and they need everybody who’s planning to deliver cargo
to keep delivering cargo. We see ourselves as a key part of the future,
and I remind the team of that periodically. “You know, some
day you’re going to tell your grandchildren that you enabled
exploration of the Solar System by doing this, as small as it may
seem.”
It’s not small to the company. It’s a huge effort for
us, but it’s very exciting. Sitting in the control center, waiting
for Antares to launch and watching the team—I was Mission Director,
so if something went wrong, I was the guy.
Wright:
We have just about a minute. Tell us about your feelings that day
and what it felt like to watch that rocket go.
Culbertson:
It was great to be back in a control center, first of all, and of
course we had a couple of aborts. That’s very familiar feelings
too. That spaceflight, that was fantastic to be that involved in it
again. Dave [David W. Thompson, Orbital founder and CEO (Chief Executive
Officer)] asked me specifically to take that role. He also asked me
to be the spokesperson at the press conferences. I don’t know
if you saw any of those or not, but that was like déjà
vu all over again. Some of the same people in the audience actually,
and all the same questions.
I think we at Orbital showed them that we can do a good job. Three
or four people in the press came up to me and used the same words
of, “We’re happy to see a company that exhibits a quiet
competence, and you guys are doing that in a great way.” If
we had problems, we explained them thoroughly. If we didn’t
launch, we told [the press] exactly what went wrong and what our plans
were. I even had to push the NASA guys and say, “they want to
know, arrange something here and let’s talk to them.”
They made the trip out here, let’s make it worth their while.
They’re not always our enemies. Being a part of that team and
watching them work is just, I mean, it’s what I live for.
Wright:
Do you feel that this is more of a partnership than it is a customer
arrangement?
Culbertson:
Yes, it’s a pretty good partnership. It’ll always be a
business arrangement to a certain extent, but we really do depend
on each other to do our jobs right, whether it’s NASA, MARS,
or us. Everybody’s got to do their job right, and it’s
like the contractor team on the Shuttle or on the Station. Yes, you
had a business relationship, but you had to make that secondary to
getting the job done because human lives are at stake. In this case,
the future of the company’s at stake. This is our biggest contract
ever, so we have to make it work.
You’re not really thinking about that during the countdown and
the actual launch itself. You’re thinking about, “This
is our hardware, it really needs to work. Did everybody do everything
right?” Apparently they did on this one. We’ve just got
to keep the same team focused and keep them operating at the same
high level, and keep the others that are coming behind them motivated
to do the same.
It’s a lot of fun to be here. I’m really enjoying my job
now. The National Security stuff is very exciting also, and there
are some complementary aspects to them in terms of the complexity
and you need to be absolutely right and absolutely successful in everything
you do. I keep reminding the team that the future of this human space
program depends on them.
Wright:
We look forward to the next launch and all the successes that are
going to follow.
[End
of Interview]